Thrust Profile (N)
1.15s Burn WindowEngineered by Cesaroni Technology, the 93G80-14A is a 29mm solid rocket motor designed for model rocketry. As an official G-class motor, it delivers a total impulse of 92.9 Ns over a 1.15 second burn window.
With an average thrust of 80.5 N and a peak of 112.2 N, it features a regressive thrust curve optimal for general sport flying. It utilizes the Skidmark propellant formulation, dictating its specific impulse and exhaust signature.
Technical Specifications
Canadian Association of RocketryMass Budget
143.2g TotalDesign wings in your spreadsheet
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